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A relaxation method for calculating transonic flows with detached bow shocks

  • Earll M. Murman
Conference paper
Part of the Lecture Notes in Physics book series (LNP, volume 19)

Keywords

Mach Number Normal Shock Transonic Flow Subsonic Region Finite Difference Procedure 
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References

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    Vincenti, W. C. and Wagoner, C. B., NACA Report 1095, 1951.Google Scholar
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    Murman, E. M. and Krupp, J. A. Lecture Notes in Physics, Vol. 8 pp 199–206, Springer-Verlag 1971.Google Scholar
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    Bailey, F. R., NASA TN D-6582, 1971.Google Scholar
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    Krupp, J. A., Ph.D. Thesis, Univ. of Washington, 1971.Google Scholar
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    Cole, J. D., Boeing Scientific Research Laboratories Document DI-82-0878, 1969.Google Scholar
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    Gothert, B. H., Transonic Wind Tunnel Testing. AGARDograph No. 49, Permagon Press. 1961.Google Scholar
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    Spreiter, J. R. and Alksne, A. Y., NACA Report 1359, 1957.Google Scholar
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    Nonweiler, T. R. F., Journal of Fluid Mech. Vol. 4, Part 2, pp 140–148 (1958).zbMATHCrossRefADSMathSciNetGoogle Scholar

Copyright information

© Springer-Verlag 1973

Authors and Affiliations

  • Earll M. Murman
    • 1
  1. 1.Ames Research CenterNASAMoffett FieldUSA

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